Boeing 717-200
Service difficulty reports · 18,771
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '717200' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '717200' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2017101707575Seat Track · corrodedSEAT TRACK RBL 44, BS 200 - 246 CORRODED. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-20-52-2R-5.SDR DALA2017101707574Shear Tie · crackedCRACKED SHEAR TIE BS 1022 BETWEEN STRINGERS 4 - 5L. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-06-2R-2, FIG 201.SDR DALA2017101707573Frame Angle · corrodedCORROSION ON FRAME ANGLE BS 908, BETWEEN LONGERONS 25R TO 26L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, AND DWG 9912243, REV JS.SDR DALA2017101707572Skin · crackedSKIN CRACKED BS 1022, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 590959-14, REV ORIGINAL, AND ETI-17-17-182, REV 1.SDR DALA2017101707571Seat Track · corrodedCORROSION ON THE RT SEAT TRACK RBL 22, BS 200 TO 257. THE SEAT TRACK WAS REPLACED IAW SRM 53-20-52-2R-5.SDR 2018F00017Skin · delaminatedDURING UNSCHEDULED MAINTENANCE CHECK, THE RT INBD SPOILER WAS FOUND TO BE DELAMINATED ON THE UPPER SURFACE.SDR DALA201101601Skin · delaminatedDURING AN UNSCHEDULED MAINTENANCE CHECK OF THE LT, OTBD SPOILER, FOUND DELAMINATION ON THE UPPER SURFACE.SDR DALA2017101607504Frame Angle · crackedCRACK ON FRAME ANGLE, BS 1053 BETWEEN LONGERONS 17 - 18L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG S2912293S, REV DL.SDR DALA2017101607526Frame · crackedCRACK ON FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R-4. PERFORMED A HFEC INSPECTION, NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDTSPM 06-10-01.001.SDR DALA2017101607524Skin · corrodedEXCESSIVE CORROSION ON THE FUSELAGE SKIN, UNDER FILLET FAIRINGS BETWEEN BS 849 - 856, LONGERONS 29R TO 28L. THE SKIN WAS REPAIRED IAW SRM 53-20-70-2R.SDR DALA2017101607522Longeron · crackedCRACKED LONGERON 7R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.SDR DALA2017101507570Access Panel · crackedFUEL ACCESS PANEL CRACKED. REPLACED THE ACCESS PANEL.SDR DALA2017101507527Light · malfunctionedEXIT LIGHT OVER AFTL EXIT, FLICKERED SEVERAL TIMES IN-FLIGHT THEN REMAINED ON. ALL OTHER CABIN EMERGENCY LIGHTS REMAINED OFF. F/A TRIED RESET, BUT WAS UNSUCCESSFUL. COULD NOT DUPLICATE, INSPECTED AND TESTED EMERGENCY LIGHTS IAW AMM 33-51, NO DEFECTS NOTED SDR DALA2017101507521Clamp · wornWORN RT CABLE CLAMP OF TAIL CONE RELEASE SYSTEM ALSO RUSTED HARDWARE ON PULLEY AT 11 HRS POSITION. THE CABLE CLAMP WAS REPLACED IAW AMM 53-52-01 AND HARDWARE ON PULLEY WAS REPLACED IAW AMM 20-00-02.SDR DALA2017101507517Frame · crackedCRACKED RT RING PAN AFT/UPPER CORNERS BS 908. : FASTENERS AND AREA DAMAGE REMOVED IAW SRM 51-41-02, 51-41-05, AND 56-20-02-2R. HFEC INSPECTION WAS ACCOMPLISHED. NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. A REPAIR WAS FABRICATED IAW SRM 56-20-02-SDR DALA2017101507516Frame · crackedCRACKED RH RING PAN AFT/LOWER CORNER BS 946, FASTENERS AND AREA DAMAGE WERE REMOVED IAW SRM 51-41-02, 51-41-05, AND 56-20-02-2R. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW NDT SPM 06-10-01.001. . REPAIR FABRICATED IAW SDR DALA2017101507515Wire · brokenBROKEN WIRES ON THE L1 DOOR SLIDE LANYARD. THE LANYARD WAS REPLACED IAW AMM 25-61-01-400-801.SDR DALA2017101507513Beam · crackedCRACKED NR 6 BEAM MID POSITION JUST AROUND BOLT AT THE FWD PASSENGER DOOR. THE DAMAGE WAS REPAIRED IAW ER/A 559578-14MA, REV ORIGINAL.SDR DALA2017101507511Structure · corrodedAFTER A CORRODED NUT WAS REMOVED, CORROSION AND SCRATCHES AT BORES WERE FOUND. BORE OF BARREL NUT NR 27 WAS REPAIRED IAW ETI-17-17-190, REV 1, AND ER/A 562336-14, REV ORIGINAL.SDR DALA2017101507510Access Panel · corrodedCORROSION COUNTERSINK ON FUEL ACCESS PANEL 141AL. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01-2R-2.SDR DALA2017101407508Floorbeam · crackedCRACKED FLOORBEAM BS 737, LBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-05, AND 51-41-02.SDR DALA2017101407505Pan · crackedCRACKED OUTER PAN ON BS 389 AND NR 5 BEAM AT FWD CARGO BAY DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R-1, FIG 201.SDR DALA2017101307477Battery Pack · inoperativeBOTH AFT (RT & LT) OVERWING EMERGENCY EXIT CABIN LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT OVERWING EMERGENCY LIGHT BATTERY IAW AMM 33-51. THE AIRCRAFT IS OK FOR SERVICE.SDR DALA2017101307476Spar Cap · crackedCRACK INDICATION ON OPEN HOLE OF SPAR CAP AFT FLANGE AT ZFS=52.767 ON THE RIGHT SIDE VERTICAL STABILIZER. REPAIRED IAW ER/A 56094-14AD, REV ORG. AND ETI-17-17-175, REV 3. SECTION II.SDR DALA2017101307475Retainer · corrodedCORROSION ON LOWER SEAL RETAINER AT FWD R1 SERVICE DOOR. THE SEAL RETAINER WAS REPLACED SRM 51-41-01-0G.SDR DALA2017101307474Beam · corrodedCORROSION ON AFT CARGO BAY LOWER DOOR FRAME BEAM BETWEEN BS 954 TO 994. THE BEAM BTW WAS REPAIRED IAW SRM 53-20-15-2R-7.SDR DALA2017101307473Frame · corrodedCORROSION OUT OF LIMITS ON FRAME BS 1022, BETWEEN LONGERONS 29 - 30L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW SRM 53-00-00-2R, PROCEDURE 2.SDR DALA2017101307471Intercostal · corrodedCORROSION ON AFT CARGO BAY INTERCOSTAL BS 1037 - 1053, LONGERONS 21 - 22L. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 5911423, REV CD.SDR DALA2017101207450Intercostal · crackedCRACK ON THE INTERCOSTAL BETWEEN BS 617 - 636, BL 0 (CEILING AREA) IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R-1, 51-41-02, AND 51-41-05.SDR DALA2017101207449Web · corrodedCORROSION ON THE WEB AT BS 201, LBL 54 OF THE L1 DOOR FRAME. THE WEB WAS REPLACED IAW SRM 51-41-01-0G, 51-41-02-0G, 51-41-05, 51-41-08, AND 53-10-15-01-2, FIG.1.SDR DALA2017101207448Seal Depressor · crackedCRACK ON THE LOWER CARGO DOOR FRAME SEAL DEPRESSOR BETWEEN BS 980 TO 985. THE LOWER SEAL DEPRESSOR WAS REPLACED IAW SRM SRM 53-20-15-0I-2, FIG. 1.SDR DALA2017101207447Seal Depressor · damagedAFT CARGO COMPARTMENT SEAL DEPRESSOR CRACKED AND WORN, ON THE AFT EDGE BETWEEN LONGERONS 24R TO 25R AND BS 994. THE SEAL DEPRESSOR WAS REPAIRED IAW SRM 53-20-15-2R-4.SDR DALA2017101107423Battery Pack · inoperativeFOUND THE AFT DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-260 IAW AMM 33-51. OPS CHECKED GOOD.SDR DALA2017101107422Battery Pack · inoperativeBOTH AFT OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPS CHECKED NORMAL IAW AMM 33-51.SDR DALA2017101107421Floor Panel · crackedCRACK ON THE FLOOR PANEL 221SF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG 201.SDR DALA2017101107412Frame · crackedCRACKED FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, PRCEDURE 4. ET, HFEC ACCOMPLISHED IAW NDT SPM 06-10-01.001 NO CRACKS FOUND AFTER DAMAGED WAS REMOVED.SDR DALA2017101107419Floor Panel · crackedCRACK ON UPPER SURFACE OF FLOOR PANEL 222AQF. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-41-02, AND SRM 53-00-00-2R-1, FIG 201.SDR DALA2017101007417Splice · crackedCRACKED SPLICE ON LEADING EDGE XRS 267, LT WING . THE SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 57-40-01-01, FIG 1, SRM 51-41-02, AND SRM 51-41-05.SDR DALA2017101007416Beam · crackedCRACK ON THE RT DOOR FRAME BEAM BS 48 AT THE NLG WHEEL WELL. THE DAMAGE WAS REMOVED, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER CUT OUT. REPAIRED IAW SRM 53-10-14, REPAIR 2.SDR DALA2017101007415Beam · crackedCRACK ON THE LT DOOR FRAME BEAM BS 48 AT THE NLG WHEEL WELL. THE DAMAGE WAS REMOVED, ET, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER CUT OUT. REPAIRED IAW SRM 53-10-14, REPAIR 2.SDR DALA2017101007414Frame Angle · crackedCRACKED FRAME ANGLE ON AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR FRAME, BETWEEN BS 1053 AND 12 O'CLOCK POSITION. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05-0G, AND 51-41-02-0G.SDR DALA2017101007392Angle · crackedCRACKED ANGLE AT 1152 BETWEEN LONGERONS 2 & 3L . THE ANGLE WAS REPLACED IAW SRM 51-41-05-0G, AND DWG 9911840, REV CR.SDR DALA2017101007391Web · corrodedCORROSION AT FLOOR WEB BS 200 BETWEEN LBL 8 - RBL 8. THE WEB WAS REPAIRED IAW SRM 51-70-10-2R, FIG 2.SDR DALA2017100907376Support · corrodedCORROSION ON PANEL SUPPORT BS 148 RBL 54. THE SUPPORT WAS REPLACED IAW SRM 51-41-02, AND SRM 51-41-08.SDR DALA2017100907375Cusp Web · corrodedCORROSION ON THE LOWER & UPPER SURFACES OF THE CUSP WEB AT BS 628. THE CORROSION WAS REMOVED. HFEC INSPECTION WAS ACCOMPLISHED. NO CRACKS FOUND AFTER TRIM OUT IAW NDTSPM 06-10-01.001. A REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55-2R-4, FIG 215.SDR DALA2017100807377Lens · looseEMERGENCY EXIT SIGN LENS FOUND LOOSE SECURED THE LENS. OK FOR SERVICE.SDR DALA2017100807374Floorbeam · corrodedCORROSION ON THE FLOORBEAM BS 200 BETWEEN RBL 9 - 44, THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-01-2, 51-40-08, 51-10-04, PAR 15, 21, 51-41-02, AND 51-41-05.SDR DALA2017100807373Pan · crackedCRACK ON RT RING PAN BS 757. REPAIRED PER B-717 SRM 56-20-02-2R-1, FIG 202.SDR DALA2017100807371Web · crackedCRACKED WEB BS 715, BETWEEN LONGERONS 11 - 15R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND 51-40-08-0G.SDR DALA2017100807370Floor Panel · crackedCABIN FLOOR PANEL 222ZF WAS FOUND CRACKED ON THE MID SECTION. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2.
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